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Analysis of thermoelastic interaction of manufacturing stresses along the interface on interlaminar delamination progression in multi-ply composite laminates

机译:多层复合层合板中沿层间界面制造应力的热弹性相互作用分析

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This paper deals with the study of interaction of manufacturing thermal residual stresses and mechanical loading in penny-shaped delaminations embedded between dissimilar,anisotropic fiber composite layers by conducting two sets of three-dimensional thermoelastic finite element analyses with and without residual stress effects.Modified crack closure integral (MCCI) techniques based on the concepts of linear elastic fracture mechanics (LEFM) have been used to calculate the distribution of individual modes of strain energy release rates (SERR) to investigate the interlaminar delamination initiation and propagation characteristics.Asymmetric variations of strain energy release rates obtained along the delamination front are caused by the overlapping stress fields due to the coupling effect of thermal and mechanical loadings.It is found that parameters such as ply sequence and orientation,thermoelastic anisotropy and material heterogeneity,and ply properties of the delaminated interface dictate the interlaminar fracture behavior of multi-ply laminated FRP composites.
机译:本文通过进行两组具有和不具有残余应力影响的三维热弹性有限元分析,研究了制造热残余应力与嵌在异种各向异性纤维复合材料层之间的便士状分层中的机械载荷之间的相互作用。基于线性弹性断裂力学(LEFM)概念的闭合积分(MCCI)技术已用于计算应变能释放速率(SERR)的各个模式的分布,以研究层间层间分层的起始和传播特性。沿分层前缘获得的能量释放速率是由于热载荷和机械载荷的耦合效应引起的重叠应力场引起的。发现层的层序和取向,热弹性各向异性和材料异质性以及层的层特性等参数接口二多层层压玻璃钢复合材料的层间断裂行为。

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